FR3021704B1 - Nacelle pour turboreacteur d'aeronef comprenant une tuyere secondaire a portes rotatives - Google Patents

Nacelle pour turboreacteur d'aeronef comprenant une tuyere secondaire a portes rotatives

Info

Publication number
FR3021704B1
FR3021704B1 FR1454927A FR1454927A FR3021704B1 FR 3021704 B1 FR3021704 B1 FR 3021704B1 FR 1454927 A FR1454927 A FR 1454927A FR 1454927 A FR1454927 A FR 1454927A FR 3021704 B1 FR3021704 B1 FR 3021704B1
Authority
FR
France
Prior art keywords
nacelle
secondary pipe
rotary doors
turboreactor
aircraft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR1454927A
Other languages
English (en)
Other versions
FR3021704A1 (fr
Inventor
Sarah Tissot
Xavier Bouteiller
Olivier Kerbler
Patrick Gonidec
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Nacelles SAS
Original Assignee
Aircelle SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to FR1454927A priority Critical patent/FR3021704B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to PCT/FR2015/051323 priority patent/WO2015181471A1/fr
Priority to EP15729539.5A priority patent/EP3149318B1/fr
Priority to RU2016150900A priority patent/RU2688082C2/ru
Priority to CA2949746A priority patent/CA2949746A1/fr
Priority to CN201580028435.XA priority patent/CN106662040B/zh
Priority to BR112016028164A priority patent/BR112016028164A2/pt
Publication of FR3021704A1 publication Critical patent/FR3021704A1/fr
Application granted granted Critical
Publication of FR3021704B1 publication Critical patent/FR3021704B1/fr
Priority to US15/364,623 priority patent/US10100780B2/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1261—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a substantially axially movable structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/40—Movement of components
    • F05D2250/42—Movement of components with two degrees of freedom
FR1454927A 2014-05-30 2014-05-30 Nacelle pour turboreacteur d'aeronef comprenant une tuyere secondaire a portes rotatives Expired - Fee Related FR3021704B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1454927A FR3021704B1 (fr) 2014-05-30 2014-05-30 Nacelle pour turboreacteur d'aeronef comprenant une tuyere secondaire a portes rotatives
EP15729539.5A EP3149318B1 (fr) 2014-05-30 2015-05-20 Nacelle pour turboréacteur d'aéronef comprenant une tuyère secondaire à portes rotatives
RU2016150900A RU2688082C2 (ru) 2014-05-30 2015-05-20 Гондола турбореактивного двигателя, содержащая сопло вторичного контура с поворотными створками
CA2949746A CA2949746A1 (fr) 2014-05-30 2015-05-20 Nacelle pour turboreacteur d'aeronef comprenant une tuyere secondaire a portes rotatives
PCT/FR2015/051323 WO2015181471A1 (fr) 2014-05-30 2015-05-20 Nacelle pour turboréacteur d'aéronef comprenant une tuyère secondaire à portes rotatives
CN201580028435.XA CN106662040B (zh) 2014-05-30 2015-05-20 包括带有旋转门的次级喷嘴的飞机涡轮喷气发动机机舱
BR112016028164A BR112016028164A2 (pt) 2014-05-30 2015-05-20 Nacela para um motor turbojato de aeronaves compreendendo um bocal secundário com portas giratórias
US15/364,623 US10100780B2 (en) 2014-05-30 2016-11-30 Nacelle for an aircraft turbojet engine comprising a secondary nozzle section with rotary doors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1454927A FR3021704B1 (fr) 2014-05-30 2014-05-30 Nacelle pour turboreacteur d'aeronef comprenant une tuyere secondaire a portes rotatives

Publications (2)

Publication Number Publication Date
FR3021704A1 FR3021704A1 (fr) 2015-12-04
FR3021704B1 true FR3021704B1 (fr) 2016-06-03

Family

ID=51417447

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1454927A Expired - Fee Related FR3021704B1 (fr) 2014-05-30 2014-05-30 Nacelle pour turboreacteur d'aeronef comprenant une tuyere secondaire a portes rotatives

Country Status (8)

Country Link
US (1) US10100780B2 (fr)
EP (1) EP3149318B1 (fr)
CN (1) CN106662040B (fr)
BR (1) BR112016028164A2 (fr)
CA (1) CA2949746A1 (fr)
FR (1) FR3021704B1 (fr)
RU (1) RU2688082C2 (fr)
WO (1) WO2015181471A1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3054266B1 (fr) * 2016-07-25 2018-08-31 Safran Nacelles Systeme d’actionnement d’un panneau de nacelle de turboreacteur
US10752371B2 (en) * 2016-09-30 2020-08-25 General Electric Company Translating nacelle wall for an aircraft tail mounted fan section
US10738737B2 (en) * 2016-11-18 2020-08-11 Rohr, Inc. Self-locking alignment at a nacelle interface
FR3074776B1 (fr) * 2017-12-13 2020-02-28 Safran Nacelles Levre d’entree d’air de nacelle pour turboreacteur
FR3075274B1 (fr) * 2017-12-14 2021-10-22 Airbus Operations Sas Turboreacteur d'aeronef comportant des moyens permettant de varier sa surface de sortie
FR3088373B1 (fr) * 2018-11-09 2021-03-19 Safran Nacelles Joint d’etancheite pour nacelle de turboreacteur d’aeronef
FR3100578B1 (fr) 2019-09-05 2021-09-24 Safran Nacelles Inverseur de poussée muni d’une cinématique à câble pour volets écopants

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3764096A (en) * 1972-02-24 1973-10-09 Rohr Industries Inc Thrust reversing apparatus
US4605169A (en) * 1983-12-27 1986-08-12 United Technologies Corporation Exhaust nozzle construction
FR2622929A1 (fr) 1987-11-05 1989-05-12 Hispano Suiza Sa Inverseur de poussee de turboreacteur a grilles,a section variable d'ejection
FR2741910B1 (fr) * 1995-11-30 1998-01-02 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes a panneau arriere articule
FR2903455B1 (fr) * 2006-07-05 2013-01-18 Airbus France Procede pour inverser la poussee produite par un ensemble propulsif d'un aeronef, dispositif pour sa mise en oeuvre, nacelle equipee dudit dispositif
FR2910937B1 (fr) * 2007-01-02 2009-04-03 Airbus France Sas Nacelle de reacteur d'aeronef et aeronef comportant une telle nacelle
FR2929998B1 (fr) * 2008-04-14 2011-08-12 Aircelle Sa Nacelle de turboreacteur a double flux
FR2946696B1 (fr) 2009-06-10 2012-04-20 Aircelle Sa Dispositif d'inversion de poussee
FR2965304B1 (fr) * 2010-09-23 2012-10-12 Airbus Operations Sas Dispositif de decharge d'air pour turboreacteur d'avion a double flux
FR2967399B1 (fr) * 2010-11-16 2012-11-02 Aircelle Sa Nacelle pour turboreacteur double flux d'un aeronef
FR2978800B1 (fr) * 2011-08-05 2014-05-23 Aircelle Sa Nacelle de turboreacteur a tuyere variable
US9103298B2 (en) * 2011-12-29 2015-08-11 Rohr, Inc. Seal for a variable area fan nozzle
GB201220378D0 (en) * 2012-11-13 2012-12-26 Rolls Royce Plc A gas turbine engine exhaust nozzle
FR3011820B1 (fr) * 2013-10-11 2017-03-31 Aircelle Sa Nacelle pour moteur d'aeronef a tuyere de section variable

Also Published As

Publication number Publication date
US20170082064A1 (en) 2017-03-23
EP3149318B1 (fr) 2018-08-22
FR3021704A1 (fr) 2015-12-04
CN106662040A (zh) 2017-05-10
CA2949746A1 (fr) 2015-12-03
RU2688082C2 (ru) 2019-05-17
EP3149318A1 (fr) 2017-04-05
CN106662040B (zh) 2019-10-08
WO2015181471A1 (fr) 2015-12-03
RU2016150900A (ru) 2018-07-02
US10100780B2 (en) 2018-10-16
RU2016150900A3 (fr) 2018-11-30
BR112016028164A2 (pt) 2017-08-22

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